DocumentCode
2554540
Title
Mutual test and diagnosis: architectures and algorithms for spacecraft avionics
Author
LaForge, Laurence E. ; Korver, Kirk F.
Author_Institution
The Right Stuff of Tahoe Inc., Reno, NV, USA
Volume
5
fYear
2000
fDate
2000
Firstpage
295
Abstract
We explain how the advantages of built-in self-test (BIST) can be surpassed by mutual test and diagnosis (MTAD). By applying techniques from system level diagnosis, MTAD substantially decreases (1) the percentage of faulty circuits misdiagnosed as good, (2) the area required to analyze the response of a circuit under test, and (3) the probability of aliasing. In addition, MTAD drives down the cost of manufacturing spacecraft avionics. The overhead of BIST hardware has been reported as low as 3.5% and as high as 15% of the total circuit area. MTAD reduces this overhead to a near-negligible fraction. Instead of an architecture whose nodes test themselves, MTAD uses an architecture whose nodes compare outputs. This approach runs at about the same speed as BIST, but with less overhead and demonstrably greater accuracy. MTAD is particularly useful for spacecraft avionics multiprocessors, wherein the assumption of a master fault-free node is questionable
Keywords
avionics; design for manufacture; design for testability; fault tolerant computing; integrated circuit testing; multiprocessing systems; space vehicle electronics; wafer-scale integration; WSI diagnosis; avionics multiprocessors; built-in self-test comparison; diagnosis architectures; fault tolerance; internal scan; manufacturing cost reduction; mutual test and diagnosis; pad level; probability of aliasing; spacecraft avionics; system level diagnosis; test architecture; test redundancy; Aerospace electronics; Aircraft manufacture; Automatic testing; Built-in self-test; Circuit faults; Circuit testing; Costs; Fault diagnosis; Manufacturing; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference Proceedings, 2000 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
0-7803-5846-5
Type
conf
DOI
10.1109/AERO.2000.878501
Filename
878501
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